Failure of tapered composites under static and fatigue tension loading
- 1 May 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (5) , 911-918
- https://doi.org/10.2514/3.12510
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- The effect of ply-drop configuration on the delamination strength oftapered composite structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Analysis for delamination initiation in postbuckled dropped-ply laminatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Delamination in tapered unidirectional glass fibre-epoxy under static tension loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Delamination of tapered composite structuresEngineering Fracture Mechanics, 1989
- Interlaminar stresses in tapered laminatesPolymer Composites, 1988
- Effect of dropped plies on the strength of graphite-epoxy laminatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987